| CPC H02J 7/0045 (2013.01) [B60L 53/16 (2019.02); B60L 53/35 (2019.02); B60L 53/62 (2019.02); B60L 53/68 (2019.02); B64F 1/35 (2024.01); H02J 7/00032 (2020.01); B60L 2200/10 (2013.01); B64C 29/0008 (2013.01)] | 18 Claims |

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1. An electric aircraft port, the port comprising:
a mating component configured to create a charging connection and a mechanical connection between an electric aircraft and a charger, wherein the charging connection enables a signal transmission between the electric aircraft and the charger; and
a control circuit configured to:
receive a control signal from a remote device;
terminate the charging connection between the charger and the electric aircraft in response to a stop request signal; and
detach the mating component from the electric aircraft to terminate the mechanical connection between the charger and the electric aircraft.
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